SAE AS7482
Studs, Corrosion and Heat Resistant Steel, UNS S66286, Tensile Strength 130 ksi, 1800 °F Solution Heat Treated, Aged Before Roll Threading Procurement Specification.
Standard:
AKA:
- AS7482
- 2011-08-16
- 1995-05-01
- Historical. Access the latest revision: AS7482B
- E-25 General Standards For Aerospace And Propulsion Systems
This specification covers aircraft quality studs amde from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286 and of 130 000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200°F.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AS7482B | 2009-09-01 | Latest | |
| AS7482A | 1996-10-01 | Historical | |
| AS7482 | 1995-05-01 | Historical |
- SAE AS 7482
- Aerospace
- Parts